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ARCTICSAT-1, 61762

Orbit data source: Space-Track

ARCTICSAT-1, 61762 is a Commonwealth of Independent States-origin payload satellite in SSO that was launched on Mon, 04 Nov 2024 UTC via a SOYUZ-2-1B launch vehicle from the Vostochny Cosmodrome (VOSTO). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

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Iframe embed code

<iframe src="https://www.satcat.com/sats-embedded/61762?theme=dark&initialShowStats=false" width="600" height="400" frameborder="0" title="Kayhan Space Satcat Satellite Viewer"></iframe>

Iframe URL

https://www.satcat.com/sats-embedded/61762?theme=dark&initialShowStats=false

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ISO8601 Format

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ISO8601 Format

Identifier

61762, 2024-199AD

Orbit

SSO

Country

CIS

Related business

Northern (Arctic) Federal University (RU)

Manufacturer

Sputniks

Mission

Operational Amateur Sci/Com

Bus & Motor

CUBESAT 3U, Unknown motor

Mass

3 kg wet, 3 kg dry

Launch date (UTC)

2024-11-04 (1 year ago)

Launch vehicle

SOYUZ-2-1B

Launch site

Vostochny Cosmodrome (VOSTO)

Object type

Payload

Rocket body

Debris

Shape & HBR

Box, 0.1 m

Radar Cross Section

0.035 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 7 hours ago

TLE from 7 hours ago

0 ARCTICSAT-1
1 61762U 24199AD  26061.78972239  .00097847  00000-0  10231-2 0  9993
2 61762  97.3110 299.8603 0003686 293.5937  66.4935 15.64137554121315

Epoch: 2026-03-02T18:57Z

TLE epoch observation values (Epoch: 2026-03-02T18:57:12.014Z)

Latitude

-0.00002°

Longitude

-145.01785°

Altitude

377.881 km

Speed

7.684 km/s

True Right ascension

19h 59m 26s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

Unknown

Longitude

Unknown

Altitude

Unknown

Speed

Unknown

Apparent Right ascension

Unknown

Apparent Declination

Unknown

Sunlit

N/A

Visualization observer readout

Local Sidereal Time

05:23:26

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

375.112 km

Perigee altitude

370.135 km

Semi-major axis

6,750.76 km

Eccentricity

0.00037

Inclination

97.311°

RAAN

299.8603°

Arg. of periapsis

293.5937°

True anomaly

66.53224°

Mean anomaly

66.4935°

Eccentric anomaly

66.51287°

Mean motion

3.91304 °/min

Orbital period

92 mins

BSTAR

0.0010231

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Other satellites on launch #199 in the year 2024 (2024-11-04 UTC)

OBJECT BF, 61788

OBJECT AT, 61776

OBJECT Z, 61758

OBJECT T, 61752

OBJECT AY, 61781

OBJECT AS, 61775

NOKHCHO, 61767 (Decayed)

TUSUR GO, 61782

OBJECT K, 61744

OBJECT AC, 61761

IONOSFERA-M 02, 61736

OBJECT E, 61739

OBJECT BD, 61786

OBJECT H, 61742

Did you know?

You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.

Click here to try in Sandbox

ARCTICSAT-1 Visibility forecast

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Span	Click to sort rows by Start time (UTC) header in descending order	Start Az.	Max El. time (UTC)	Max El. Az.	Max El.	End time (UTC)	End Az.
5 mins	2026-03-03 04:43:29.767Z	8.176° NNE	2026-03-03 04:45:29.767Z	322.159° NNW	44.09°	2026-03-03 04:48:29.767Z	196.424° SSW

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Co-orbital & Co-planar RSOs

Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions

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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings

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Check out ARCTICSAT-1, 61762 on other resources

View ARCTICSAT-1, 61762 on NASA - NSSDCA Website

View ARCTICSAT-1, 61762 on Heavens-Above

View ARCTICSAT-1, 61762 on Keep Track

View ARCTICSAT-1, 61762 on Celestrak

View ARCTICSAT-1, 61762 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

Documentation

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